View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 56046U 26145.31950549 +.00000000 +00000-0 +35802-3 0 00009
2 56046 87.9106 233.3119 0002107 106.1871 253.9492 13.16593380 03
| Epoch (UTC): | 25 May 2026 07:40:05 |
| Eccentricity: | 0.0002107 |
| inclination: | 87.9106° |
| perigee height: | 1196 km |
| apogee height: | 1199 km |
| right ascension of ascending node: | 233.3119° |
| argument of perigee: | 106.1871° |
| revolutions per day: | 13.16593380 |
| mean anomaly at epoch: | 253.9492° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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